gusucode.com > Electric_Aircraft_Simscape > Electric_Aircraft_Simscape_R19a/Airtaxi_VTOL/Scripts_Data/ssc_airvtol_elec_props.m
function [mass, wing_area, cd, cl] = ssc_airvtol_elec_props(aircraft_type) % Returns mass, equivalent wing area, coefficient of drag, coefficient of % lift properties for a requested aircraft type. % Copyright 2017-2019 The MathWorks, Inc. % Data for single seat aircraft similar to Airbus E-Fan aircraft.singleseatehang184.mass = 210; % kg without battery aircraft.singleseatehang184.wing_area = 4; % m^2 aircraft.singleseatehang184.cl = 0.5; % Lift coefficient aircraft.singleseatehang184.cd = 0.05; % Drag coefficient % Data for double seat aircraft similar to Alpha Electro aircraft.doubleseatworkhorsesurefly.mass = 400; % kg without battery aircraft.doubleseatworkhorsesurefly.wing_area = 9; % m^2 aircraft.doubleseatworkhorsesurefly.cl = 0.45; % Lift coefficient aircraft.doubleseatworkhorsesurefly.cd = 0.055; % Drag coefficient field_name = lower(strrep(strrep(strrep(strrep(... aircraft_type,' ',''),... '-',''),... '(',''),... ')','')); % Assign output mass = aircraft.(field_name).mass; wing_area = aircraft.(field_name).wing_area; cd = aircraft.(field_name).cd; cl = aircraft.(field_name).cl;